Browse By Repository:

 
 
 
   

Design and analysis of landing gear trainer system for aviation maintenance training purposes

Azhari, Nur Nadiah (2021) Design and analysis of landing gear trainer system for aviation maintenance training purposes. Project Report. Universiti Teknikal Malaysia Melaka, Melaka, Malaysia. (Submitted)

[img] Text (24 Pages)
Design and analysis of landing gear trainer system for aviation maintenance training purposes.pdf - Submitted Version

Download (5MB)
[img] Text (Full text)
Design and analysis of landing gear trainer system for aviation maintenance training purposes.pdf - Submitted Version
Restricted to Repository staff only

Download (16MB)

Abstract

The Landing Gear Mechanism Trainer is an extremely useful piece of equipment for aircraft repair schools' hands-on instruction. It is critical to guarantee that trainees comprehend the theory and are also well equipped to maintain the landing gear system in the best possible condition and in accordance with cun-ent safety regulations. The device can also be used in the lecture or during ground school course training. In this field, there is a clear need for aviation maintenance engineers and technicians and to be trained. However, most aviation maintenance school in Malaysia do not own their landing gear trainer system as part of the teaching mechanism because it is too expensive. However, the cost is varying greatly with the material and system used for the landing gear trainer system. The product per performance has greatly improved because of the advanced design work. This project report discussed about market feasibility and the design parameters required to construct a hydraulic landing gear trainer system equipped with retractable main and nose landing gear by applying the previous study of landing gear trainer system model. By using engineering methods which are a market survey, House of Quality (HoQ), and Morphological Method, three conceptual designs of hydraulic landing gear trainer system were produced. The.final design was selected by using the engineering approach which is Weighted Decision Matrix (WDM). The final design was designed using CA TIA software, and two analysis was done which are Finite Element Analysis (FEA) for the main landing gear structure and the body of the landing gear trainer system. At the end of this project, detailed design including the analysis of the hydraulic landing gear trainer system was produced.

Item Type: Final Year Project (Project Report)
Uncontrolled Keywords: Airplanes, Landing gear, Design and construction, Landing gear Finite element method
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics
Divisions: Library > Final Year Project > FKM
Depositing User: Sabariah Ismail
Date Deposited: 14 Jul 2022 07:19
Last Modified: 15 Jul 2022 02:15
URI: http://digitalcollection.utem.edu.my/id/eprint/26630

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year